US20230121923A1 - Support module for a fan and fan having a corresponding support module - Google Patents

Support module for a fan and fan having a corresponding support module Download PDF

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Publication number
US20230121923A1
US20230121923A1 US17/792,359 US202017792359A US2023121923A1 US 20230121923 A1 US20230121923 A1 US 20230121923A1 US 202017792359 A US202017792359 A US 202017792359A US 2023121923 A1 US2023121923 A1 US 2023121923A1
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United States
Prior art keywords
support module
struts
fan
nozzle plate
impeller
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Pending
Application number
US17/792,359
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English (en)
Inventor
Frieder Loercher
Sandra Hub
Matthias GOELLER
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Ziehl Abegg SE
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Ziehl Abegg SE
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Assigned to ZIEHL-ABEGG SE reassignment ZIEHL-ABEGG SE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GOELLER, Matthias, HUB, SANDRA, LOERCHER, FRIEDER
Publication of US20230121923A1 publication Critical patent/US20230121923A1/en
Pending legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/626—Mounting or removal of fans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/08—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226—Fan casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226—Fan casings
    • F04D29/4233—Fan casings with volutes extending mainly in axial or radially inward direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226—Fan casings
    • F04D29/4246—Fan casings comprising more than one outlet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
    • F04D29/444—Bladed diffusers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/54—Building or constructing in particular ways by sheet metal manufacturing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/50—Inlet or outlet
    • F05D2250/52—Outlet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved

Definitions

  • the present disclosure relates to a support module for a fan, which includes a motor and a fan impeller driven in rotation by the motor, in particular for a radial or diagonal fan, for fastening the fan impeller between a nozzle plate on the inflow side and a base plate lying opposite the nozzle plate at a distance, wherein the motor is non-rotatably mounted with the fan impeller on or in the base plate and is held on the nozzle plate by means of struts extending between the base plate and the nozzle plate.
  • the disclosure also relates to a fan with a corresponding support module.
  • this is a support device that is used for fastening a motor with a fan impeller, with the motor and the fan impeller being usually fastened to a base plate of the support device. While the motor is non-rotatably arranged at its stator on the support device, the fan impeller rotates with the rotor of the motor.
  • the arrangement of the base plate of the support device with motor and fan impeller is mechanically connected to the nozzle plate, which usually includes an inlet nozzle, and is, in other words, held on the nozzle plate. Struts that extend between the base plate and the nozzle plate are usually used for this purpose. These are fasteners in the broadest sense that space the nozzle plate from the base plate and stabilize the arrangement with the interposed fan impeller. Due to the arrangement of the struts, the arrangement of the components discussed above is to be understood as a structural unit.
  • the support devices known from practice which provide the attachment of radial or diagonal fan impellers to the nozzle plate, are problematic insofar as the connecting struts extend downstream from the air outlet and, due to their provision, cause losses in efficiency, losses in air output and/or an increase in noise; at least they do not increase the static efficiency.
  • the arrangement known from practice often requires a not inconsiderable amount of space, far from a compact design.
  • Fans with known support devices have a pronounced, disruptive sub-harmonic noise, especially at operating points of high static pressure increases, since known support devices do not stabilize the flow downstream of the impeller.
  • the object of the present disclosure is therefore to at least reduce the aforementioned disadvantages.
  • the known support device is to be optimized into a support module by the special design of its struts and possibly also of the motor support plate or of the base plate in such a way that the losses and the increase in noise are minimal, with the aim being to increase the efficiency and the air output as much as possible.
  • the supporting function of the support module in particular when using special struts, should at least be maintained, if not even improved, and the support module should be compact when viewed in the radial direction.
  • a correspondingly optimized fan is to be specified, which includes a support module according to the disclosure.
  • the fan should have a significantly higher static efficiency than in the prior art, in particular when using a so-called GR module of the “spider” type.
  • the support struts of such a GR module are usually formed from round material. The occurrence of a sub-harmonic rotational tone should be shifted to higher pressures compared to the prior art or be significantly reduced in a relevant operating range.
  • the aforementioned object is achieved with reference to the support module by means of the features of claim 1 .
  • the generic support module is characterized in that the struts are adjusted to the flow emerging from the fan impeller with a compact design.
  • strut is to be understood in the broadest sense within the framework of the teaching, which is initially claimed in a very general manner. These are stabilizing spacers between the base plate supporting the motor and the fan impeller, and the nozzle plate.
  • the struts should form a compact unit due to their rigidity/strength and their number and distribution around the fan impeller and at least reduce, if possible eliminate, the disadvantages occurring in the prior art due to their adaptation to the flow exiting the fan impeller.
  • the struts can be flat, planar components as well as profiled components, with different types of struts being able to be combined with one another. It is also conceivable that one type of strut replaces another type of strut.
  • the struts can have a curvature and/or a varying thickness in cross-section.
  • their shape and orientation are adjusted to the flow conditions after the air has exited radially from the fan impeller. The adjustment allows the flow to be stabilized and the efficiency can be increased and the sub-harmonic noise reduced, depending on the specific adjustment.
  • the struts are advantageously profiled, as a result of which the aforementioned adaptation to the air flow can be implemented.
  • the struts can have approximately the same or a similar cross-sectional contour as the blades of the fan impeller.
  • the struts have an upstream edge and a downstream edge.
  • the cross-section of the struts on the inflow side tends to have rounded edges, in contrast to the outflow-side edges, similar to an airfoil, in order to ensure an aerodynamically stable behavior of the struts with regard to varying angles of attack.
  • the struts have convexly curved surfaces on the suction side and concavely curved surfaces on the pressure side.
  • the profile struts Compared to an imaginary radial, the profile struts have a different angle at their inflow edge than at their outflow edge, which results from their curvature.
  • the leading edge and trailing edge angles are designed in such a way that the efficiency of the fan is high and the noise generated by the fan is low.
  • the struts are arranged radially outside the air outlet of the fan impeller on the outflow side. In a further embodiment, the struts are parallel to the impeller axis. This allows the installation space to be minimized.
  • the number of struts can vary. At least four struts should be provided, it being possible to also provide six to ten struts depending on the required stability, depending on the size and intended use of the support module or of the fan comprising the support module.
  • the struts have a supporting function, namely hold the base plate with the motor and the impeller on the nozzle plate.
  • the provision of the struts can be used to promote the flow, in accordance with the specific configuration of the struts discussed above.
  • the struts can be made from different materials and accordingly using different processes.
  • the struts can be produced as aluminum profiles or sheet steel using the extrusion process, or as plastic profiles using the injection molding process. It is important to note whether the struts are the only components that take on the supporting function or whether additional stabilizing and therefore supporting components are provided.
  • side parts can be provided in or near the corner regions of the nozzle plate, which extend between the nozzle plate and the base plate. These can be independent components that are connected to the nozzle plate and the base plate. These side parts are arranged radially outside the air outlet of the fan impeller on the outflow side and, in an embodiment, parallel to the impeller axis.
  • the side parts are, in an embodiment, arranged at a small distance from the optionally corresponding struts, such that the side parts are aligned at their leading edges with the corresponding struts at their trailing edge at a small distance, so that the side parts and struts with their leading edges and trailing edges form an aerodynamically effective unit.
  • the side parts may be arranged close to the corner regions between the nozzle plate and the base plate and/or close to the struts, for example directly adjacent to them.
  • the side parts can be designed as flat plastic injection-molded parts or as flat metal sheets, with stabilizing embossing, beads, etc. being able to be provided. In and embodiment, at least four of these side parts are provided, with six to ten side parts, for example eight side parts, being provided alone or in addition to the struts discussed above, depending on the size and use of the support module.
  • the side parts can have a supporting function and hold the base plate and the motor with the impeller on the nozzle plate. They should also stabilize the air flow and thereby increase efficiency and reduce sub-harmonic noise as much as possible.
  • the profiled struts and the rather flat side parts are connected to one another in pairs, by means of suitable connecting means, resulting in a specific arrangement and alignment of the struts and side parts provided in pairs. Due to this measure, the arrangement of the strut and side part acts as an aerodynamic unit and can promote the flow.
  • the struts and/or side parts may have the smallest possible distance from their inflow edges to the trailing edges of the impeller blades. This again favors the compact design with favorable flow conditions.
  • the struts and side parts have attachment means at their axial ends for attachment to corresponding attachment regions of the base plate and to the nozzle plate, the connection being made by screws, rivets, gluing or welding.
  • a firm connection is essential to bring about the required stability or rigidity.
  • these components have an edge region with folded edges that stiffen or stabilize the two plates. On top of that, the folded edges provide ideal fastening regions for the struts and/or the side parts.
  • the base plate and, if necessary, the nozzle plate can be made of sheet metal or plastic, using suitable manufacturing processes as a basis.
  • the base plate can have a square or polygonal contour with chamfered corners, in which case the contour can in principle also be rectangular.
  • a contour with chamfered corners may be used when the fan comprising the support module is installed in an air duct or the like with axial air routing.
  • the base plate of the support module extends radially over the entire circumference by at least 10 % over the entire impeller or over the base disk of the impeller.
  • the base plate of the support module does not have any openings or openings that are relevant to flow technology within its radial outer contour.
  • the radial extension of the nozzle plate may define the radial installation space of the support module. This is due to the specific arrangement and design of the struts and side parts.
  • the fan according to the disclosure is equipped with a support module of the type discussed above, as a result of which the efficiency losses, air output losses and noise increase occurring in the prior art due to the necessary provision of struts can be reduced, if not even eliminated.
  • a fan with the support module according to the disclosure is also extremely stable with a compact design.
  • FIG. 1 shows, in a perspective view seen from the inflow side, an exemplary embodiment of a fan with a support module according to the disclosure
  • FIG. 2 shows, in an axial top view in a planar section seen from the outflow side, the fan with support module from FIG. 1 ,
  • FIG. 3 shows, in a perspective view from the side in a section on a plane through the axis, the embodiment of a fan with support module according to FIGS. 1 and 2 ,
  • FIG. 4 shows, in a perspective view, seen from the inflow side, a further exemplary embodiment of a fan with a support module according to the disclosure, the support module not having any side plates,
  • FIG. 5 shows, in an axial top view in a planar section seen from the outflow side, the fan with support module from FIG. 4 ,
  • FIG. 6 shows, in an axial top view in a planar section seen from the outflow side, the fan with support module from FIGS. 4 and 5 ,
  • FIG. 6 a shows a detailed view of FIG. 6 , wherein angle values are also shown schematically
  • FIG. 7 shows, in a perspective view seen from the inflow side, an exemplary embodiment of a fan with a support module according to the disclosure having 4 profiled struts,
  • FIG. 8 shows, in schematic diagrams, the representation of the progression of the static pressure increases of a fan with standard suspension and of a fan with a support module according to the disclosure at constant speed
  • FIG. 9 shows, in schematic diagrams, the representation of the progression of the static efficiencies of a fan with standard suspension and of a fan with a support module according to the disclosure at constant speed
  • FIG. 10 shows, in schematic diagrams, the representation of the progression of the suction-side noise power levels of a fan with standard suspension and of a fan with a support module according to the disclosure at constant speed
  • FIG. 11 shows, in schematic diagrams, the representation of spectra of the suction-side noise pressure of a fan with standard suspension and of a fan with a support module according to the disclosure at constant speed and the same volumetric flow rate, and
  • FIG. 12 shows, in an axial plan view in a planar section seen from the inflow side, the fan with support module according to FIGS. 4 to 6 , installed in an air duct.
  • FIG. 1 shows, in a perspective view seen from the inflow side, an exemplary embodiment of a fan with a support module 1 according to the disclosure.
  • the fan impeller 3 which may be of radial or diagonal design, is visible on the inside.
  • the inlet nozzle 2 attached to a nozzle plate 5 can also be seen on the inflow side.
  • the support module 1 includes a base plate 6 and 8 lateral struts 8 radially outside (outflow side) of the air outlet of the fan impeller 3 .
  • the struts are referred to below as profile struts 8 due to their design.
  • the fan impeller 3 consists essentially of a base disk 9 , a cover disk 19 and blades 18 extending in between.
  • side parts 7 designed as side plates are present, which have a supporting function, namely they represent the supporting connection between the nozzle plate 5 and the base plate 6 .
  • the number of side plates 7 may be four.
  • the profile struts 8 may be formed from plastic.
  • the profile struts 8 and the side plates 7 cover part of the outflow region, which stabilizes the flow.
  • the static efficiency of the fan is improved, particularly in the regions of the characteristic curve with high pressure.
  • the side parts 7 may be made of sheet metal, are flat in the exemplary embodiment, that is to say they consist essentially of a one-piece continuous flat region. This is beneficial, though not required, for simple and cost-effective production of the support module 1 and its side parts 7 .
  • Fastening provisions 23 and 24 are provided for connecting the side parts 7 to the nozzle plate 5 and base plate 6 , respectively.
  • fastening provisions 25 and 26 for connecting the profile struts 8 to the nozzle plate 5 and the base plate 6 are formed.
  • the connection can be made in particular by screws, rivets, but also by welding.
  • the nozzle plate 5 made of sheet metal has a folded region 22 on its outer edge, which stabilizes the nozzle plate 5 and into which parts of the fastening provisions 23 and 25 are integrated.
  • the base plate 6 made of sheet metal has a folded region 27 on its outer edge, which stabilizes the base plate 6 and into which parts of the fastening provisions 24 and 26 are integrated.
  • the bottom plate 27 may be molded from plastic.
  • the sheet metal 6 on the side of the base disk extends radially up to the profile struts 8 and the side parts 7 .
  • FIG. 2 shows the fan with support module 1 according to FIG. 1 in axial view from above and in a planar section, as seen from the outflow side.
  • the essentially flat, supporting side parts 7 have an inflow-side edge 12 and an outflow-side edge 13 .
  • the profile struts 8 are not flat, but rather have approximately the cross-sectional contour of an airfoil. This means that they have a curvature and a non-constant thickness and their shape and orientation are adjusted to the flow conditions that occur after the air has exited the impeller 3 in the radial direction to the outside.
  • the blades 18 of the impeller 3 which are also profiled, have the inflow edges 10 and the outflow edges 11 .
  • the profile struts 8 have inflow edges 14 and outflow edges 15 .
  • the inflow edges 14 are, seen in cross section, rather round, similar to an airfoil, in order to ensure aerodynamically stable behavior of the profile struts 8 relative to different angles of attack. They have convexly curved suction-side surfaces 42 and concavely curved pressure sides 43 . Compared to an imaginary radial, the profile struts have a different angle at their inflow edge 14 than at their outflow edge 15 , which provides their curvature, seen in the cross section.
  • leading edge and trailing edge angles are designed in such a way that the efficiency of the fan is high and the noise generated by the fan is low.
  • the leading edges 12 of the flat side part 7 are not rounded, since the side part 7 is a flat sheet metal. However, the flat side parts 7 are aligned at their leading edges 12 exactly with corresponding profile struts 8 at their trailing edges 15 with a small distance, so that the side parts 7 with the corresponding profile struts 8 optimally act as an aerodynamic unit with leading edges 14 and trailing edges 13 .
  • the aerodynamically shaped profile struts 8 run parallel to the fan axis, which runs perpendicular to the plane of the drawing. Since the profile struts 8 in the exemplary embodiment are not supporting and may be made of plastic injection molding, a different path would also be conceivable, for example not parallel to the axis or with a variable cross section.
  • Fastening provisions 17 of the nozzle plate 5 or of the fan for fastening to a higher-level system such as an air-conditioning device or an air duct can be seen on the nozzle plate 5 .
  • the support module 1 essentially does not protrude beyond the nozzle plate 5 in a viewing direction parallel to the axis, as shown here, and is therefore particularly compact when viewed in the radial direction and therefore requires little installation space.
  • the support module 1 has an approximately rectangular, approximately square, cross section of width w ( 37 ) (in the case of a rectangular cross section, w is the larger width) W( 37 ) is, in an embodiment, no greater than 1.25 times the mean diameter of the trailing edges 11 of the blades 18 of the impeller 3 with respect to the fan axis.
  • FIG. 3 shows, in a perspective view seen from the side and in a section on a plane through the axis, the exemplary embodiment of a fan with support module 1 according to FIGS. 1 and 2 .
  • air is sucked in from the right through the inlet nozzle 2 into the impeller 3 and conveyed radially outwards as a result of the rotation before it flows past the profile struts 8 and side plates 7 out of the support module 1 .
  • the impeller 3 with the blades 18 extending between the base disk 9 and the cover disk 19 is driven by a motor 4 , shown schematically.
  • the motor 4 is connected to the impeller 3 on the rotor side and fixed to the base plate 6 on the stator side.
  • the motor 4 is fastened to the base plate 6 in a central region 31 which has, in an embodiment, a recess into which the motor 4 is inserted. Possible means for centering and fastening the motor 4 are provided.
  • the inlet nozzle 2 is fastened to the nozzle plate 5 or can also be molded directly into the nozzle plate 5 , for example by means of a deep-drawing process.
  • the nozzle plate 5 has a folded region 22 which stabilizes the nozzle plate 5 and can be integrated into the fastening provisions 23 and 25 .
  • the folded region 22 also has a function for the flow conditions and thus for air output and efficiency.
  • FIG. 4 shows a further exemplary embodiment of a fan with a support module 1 according to the disclosure in a perspective view seen from the inflow side.
  • the support module 1 has no side plates.
  • the profile struts 8 assume the supporting function and hold the base plate 6 , the motor and the impeller 3 on the nozzle plate 5 .
  • the profile struts 8 may be made of metal.
  • the design of the profile struts 8 as extruded aluminum profiles has proven to be particularly favorable and effective. However, it is also conceivable to manufacture them from high-strength plastic, cast aluminum or sheet steel.
  • Extruded aluminum profiles in particular can be connected to the nozzle plate 5 or the base plate 6 by directly screwing in suitable screws through the metal sheet of the nozzle plate 5 or the base plate 6 (not shown).
  • the impeller 3 with the base disk 9 , the cover disk 19 and the blades 18 may be made in one piece by plastic injection molding. Other types of impellers are also conceivable, for example by welding steel or aluminum.
  • the lateral profile struts 8 are made of sheet metal.
  • a metal sheet can be curved or folded in a suitable manner in order to realize a profile shape or at least the curved center line of the profile shape, seen in a cross section analogously to FIG. 2 .
  • FIG. 5 shows the fan with support module 1 according to FIG. 4 in an axial top view and in a planar section as seen from the inflow side.
  • the rotor of the motor 4 and the attachment of the base disk 9 of the impeller 3 to the motor 4 can be seen in the center.
  • the aerodynamically advantageous design of the cross sections of the profile struts 8 can be clearly seen, similar to the design of airfoil cross sections, as also described with reference to FIG. 2 .
  • the air flowing out radially from the impeller 3 flows with low loss on the profile struts 8 , first via their leading edge regions 14 and then via the thin trailing edge regions 15 from the support module 1 .
  • the profile struts 8 ensure through their design in interaction with the nozzle plate 5 and the base plate 6 a stabilization of the flow inside the support module 1 and thus an increase in efficiency and/or a reduction in noise, at least a sub-harmonic noise (noise in a frequency range below the blade repetition frequency, see also the description of FIG. 11 ).
  • the outer contour of the base plate 6 resembles a square with chamfered corners 45 in an axial plan view. It can also have an approximately rectangular contour. The contouring with the chamfered corners 45 is particularly advantageous if the fan with the support module 1 according to the disclosure is installed in an air duct or the like with axial air routing, see also FIG. 12 .
  • the base plate 6 of the support module 1 extends, viewed in the radial direction, continuously and over the entire circumference over the outer contour of the base disk 9 of the impeller 3 . It may extend radially over the entire circumference without interruption by at least 10% over the base plate 9 of the impeller 3 , in a further embodiment, it extends over the entire circumference without interruption by at least 10% radially over the entire impeller 3 including blades 18 and cover plate 19 .
  • the base plate 6 has no significant, aerodynamically relevant openings or breakthroughs (this does not include boreholes, cable breakthroughs, gaps due to manufacturing tolerances or the like)
  • FIG. 6 shows the fan with support module 1 according to FIGS. 4 and 5 in an axial top view and in a planar section as seen from the outflow side.
  • the trailing edges 11 of blades 18 of the impeller 3 have a relatively small distance from the inflow edges 14 of the profile struts 8 , which is advantageous for the radial compactness of the support module 1 and thus of the fan, and is also advantageous for achieving a high level of efficiency.
  • the blades 18 of the impeller 3 protrude with their leading edges 10 radially inward beyond the inner edge of the cover disk 19 .
  • the trailing edges 15 of the profile struts 8 do not protrude radially beyond the radial outer contour of the nozzle plate 5 , namely the radial extension of the nozzle plate 5 defines the radial installation space of the compact support module 1 and thus of the fan.
  • Fastening means 17 for fastening the fan to a higher-level system are provided on the nozzle plate 5 .
  • FIG. 6 a shows a detailed view of FIG. 6 , wherein angle values are also shown schematically on a profile strut 8 , namely the leading edge angle ⁇ 46 at the leading edge 14 and the trailing edge angle ⁇ 47 at the trailing edge 15 .
  • the leading edge angle ⁇ 46 is, as seen in one section on a plane perpendicular to the axis correspond to the representation according to FIG. 6 a , the angle between the local circumferential direction U 48 and the profile center line at the inflow edge 14 of a profile strut 8 .
  • the trailing edge angle ⁇ 47 corresponds to a section on a plane perpendicular to the axis 6 a , the angle between the local circumferential direction U 48 and the profile center line at the trailing edge 15 of a profile strut 8 .
  • the leading edge angle ⁇ 46 and the trailing edge angle ⁇ 47 are optimally adjusted to the flow emerging from the impeller 3 .
  • ⁇ 46 is, in an embodiment, not equal to ⁇ 47 , in a further embodiment a 46 is greater than ⁇ 47 , an in a further embodiment by at least 10° greater.
  • ⁇ 46 and ⁇ 47 are, in an embodiment, smaller than 45°.
  • FIG. 7 shows a perspective view of a further exemplary embodiment of a fan with a support module 1 according to the disclosure, seen from the inflow side.
  • the support module 1 in this embodiment has only four profile struts 8 , namely no freestanding profile struts without assigned side plates. All four profile struts 8 are assigned to a side plate 7 .
  • the side plates 7 and the associated profile struts 8 are connected to one another with connecting elements 16 in order to ensure better alignment of the side plates 7 and the profile struts 8 to one another.
  • the lateral profile struts 8 are made of sheet metal.
  • a metal sheet can be curved or folded in a suitable manner in order to realize a profile shape or at least the curved center line of the profile shape, seen in a cross section analogously to FIG. 6 a .
  • the leading edge angle ⁇ 46 and the trailing edge angle ⁇ 47 are to be selected as previously described with reference to FIG. 6 in order to achieve high efficiencies and low noise emissions.
  • FIG. 8 shows the representation of the progression of the static pressure increases of a fan with standard suspension and of a fan with a support module according to the disclosure at constant speed.
  • This representation illustrates the mode of operation of a support module according to the disclosure by comparing a characteristic curve of a fan with a support module according to the disclosure with a characteristic curve of an otherwise identical fan, in particular with the same impeller and the same motor, but in which the housing is replaced by a standard motor suspension, for example consisting of aerodynamically largely neutral round metal struts.
  • Curve 20 shows the course of the static pressure increase for the fan with standard motor mounting (reference fan) as a function of the volumetric flow rate.
  • the fan with the support module according to the disclosure has the characteristic curve 21 for the static pressure increase as a function of the volumetric flow rate.
  • the dotted line 28 shows an exemplary volumetric flow, which is also used as a basis for the following descriptions of the figures.
  • FIG. 9 shows a schematic representation of the curves of the static efficiencies as a function of the volumetric flow rate of a fan with standard suspension and a fan with a support module according to the disclosure at a constant speed.
  • the static efficiency achieved in each case is plotted as a function of the volumetric flow at constant speed.
  • the dashed efficiency curve 29 is obtained with measurements of a backward-curved centrifugal fan with standard suspension (reference fan), whereas the solid efficiency curve 30 is obtained with measurements of the same fan but using a support module according to the disclosure instead of a standard suspension. It is easy to see that the efficiency is noticeably increased by a support module according to the disclosure, particularly in regions with medium to low volume flows, that is to say with rather high static pressure increases (cf. FIG. 9 ).
  • the improvement tends to be less. In the region of medium to low volume flows or high static pressure increases, the improvement is a few percentage points, in particular at the point of maximum increase it is at least 2 percentage points or at least 3% relative.
  • the dotted line 28 shows the same exemplary volume flow that is also used in FIG. 8 . At this volume flow, the static efficiency is increased by 3 percentage points or about 4% relatively by using a support module according to the disclosure instead of a standard suspension from about 74.5% to about 77.5%
  • FIG. 10 shows the curves of the suction-side noise power level of a fan with standard suspension and a fan with a support module according to the disclosure at the same and constant speed.
  • the dashed curve 32 represents the progression of the suction-side noise power of the reference fan as a function of the air volume flow
  • the solid curve 33 represents the suction-side noise power of the otherwise identical fan but with the support module according to the disclosure instead of a standard suspension.
  • Noise power values for both fans are approximately the same over large regions of the characteristic curve, but are somewhat higher in the case of the fan with a support module according to the disclosure.
  • FIG. 11 shows the representation of spectra of the suction-side noise pressure of a fan with standard suspension and a fan with a support module according to the disclosure at constant speed and at the same volumetric flow rate 28 , which is shown in FIGS. 8 - 10 .
  • the dashed curve 39 shows the noise pressure spectrum of the reference fan and the solid curve 40 shows the noise pressure spectrum of the fan with the support module according to the disclosure at the volumetric flow rate 28 ( FIGS. 8 - 10 ).
  • the frequency resolution in the diagram shown is 3.125 Hz. With other frequency resolutions, however, the same qualitative effects can be seen.
  • the three frequencies 34 plotted are the first, second and third harmonics of the blade repetition rate of the fan impeller.
  • the noise at the first harmonic of the blade repetition frequency is also referred to as a rotary tone.
  • the noise pressure is significantly increased both for the reference fan (curve 39 ) and for the fan with the support module according to the disclosure (curve 40 ) compared to the general trend of the curves, with the noise pressure in particular at the first blade repetition frequency for the fan with the support module according to the disclosure being higher than for the reference fan. This is due in particular to the interaction of the impeller blades with the side plates and/or the profile struts.
  • the increase in the noise pressure curves in the form of regions of excessive increase 41 is referred to as sub-harmonic noise.
  • sub-harmonic noise In the case of backward-curved fans, it regularly occurs at a frequency of around 60%-90% of the first blade repetition frequency, particularly at operating points with higher static pressure increases.
  • the sub-harmonic noise which is generally dependent on the volumetric flow rate, is significantly reduced at the illustrated volumetric flow rate for the fan with a support module according to the disclosure, in the example shown by around 7-8 dB, generally by 1-15 dB, depending on the volumetric flow rate and frequency resolution.
  • the frequency of the sub-harmonic noise is also shifted slightly, by about 5%-20% of the first blade repetition frequency.
  • This reduction and frequency shift of the sub-harmonic noise at operating points with medium to low volumetric flow rate and rather large static pressure increases is caused by a flow stabilization due to the support module according to the disclosure.
  • the remaining noise for example the noise at a harmonic of the blade repetition frequency 34 or the broadband noise, can be higher or lower in a fan with a support module according to the disclosure than in the reference fan. Only the reduction of the sub-harmonic noise in the fan with housing is decisive for the description of the mode of action.
  • the noise at the first harmonic of the blade repetition frequency is increased in the fan with the support module according to the disclosure compared to the reference fan.
  • this noise can be reduced with active noise canceling, namely the cancellation of noise by introducing out of phase noise. This is technically simple, since the blade repetition frequency can be easily determined when the fan speed is known.
  • FIG. 12 shows the fan with support module 1 according to FIGS. 4 to 6 , installed in an air duct 35 , in an axial top view and in a planar section as viewed from the inflow side.
  • the inner fan impeller 3 with blades 18 and the base disk 9 and further out the eight profile struts 8 are visible in this figure.
  • the support module 1 has at least approximately 90° rotational symmetry with respect to the fan axis.
  • the support module 1 has a width w ( 37 ) in the section shown or in an axial plan view.
  • the width is determined by the side length of the smallest square defined around the support module 1 in a section on a plane perpendicular to the axis or in an axial plan view.
  • the width w ( 37 ) of the support module 1 is, in an embodiment, 1.15-1.3 times the mean diameter D of the trailing edges 11 of the blades 18 of the fan impeller 3 , which expresses the radial compactness of the support module 1 in relation to the impeller 3 . If the width w is variable in different sectional planes, the maximum width w seen over the entire axial height of the support module 1 must be used for the evaluation, without taking the nozzle plate into account.
  • the width s ( 38 ) of the air duct 35 assigned to a fan is, in an embodiment, in the range of 1.2 times to 1.8 times the width w ( 37 ) of the associated support module 1 or in the range of 1.5 times to 2.3 times the average diameter D of the trailing edges 11 of the blades 18 of the fan impeller 3 .
  • the ratio s/w of the width s ( 38 ) of the air duct 35 assigned to a fan and the width w ( 37 ) of the associated support module 1 is less than 1.4, it can be advantageous to provide chamfered corners 45 on the support module 1 so that the out-flowing air in the axial direction has more flow surface between the base plate 6 and the air duct wall 36 .

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
US17/792,359 2020-01-14 2020-12-04 Support module for a fan and fan having a corresponding support module Pending US20230121923A1 (en)

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DE102020200363.7 2020-01-14
DE102020200363.7A DE102020200363A1 (de) 2020-01-14 2020-01-14 Tragmodul für einen Ventilator und Ventilator mit einem entsprechenden Tragmodul
PCT/DE2020/200107 WO2021143971A1 (de) 2020-01-14 2020-12-04 Tragmodul für einen ventilator und ventilator mit einem entsprechenden tragmodul

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EP (1) EP4090852A1 (de)
JP (1) JP2023510519A (de)
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DE102022124201A1 (de) * 2022-09-21 2024-03-21 Ebm-Papst Mulfingen Gmbh & Co. Kg Radialventilator mit nachrüstbaren Luftleitsegmenten

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EP4090852A1 (de) 2022-11-23
JP2023510519A (ja) 2023-03-14
BR112022012984A2 (pt) 2022-09-13
CN115053072A (zh) 2022-09-13
DE102020200363A1 (de) 2021-07-15
WO2021143971A1 (de) 2021-07-22

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